Composite laminate having a damping interlayer and method of making the same

Patent metadata

Field	Value
Publication number	US-9511571-B2
Application number	US-65662607-A
Country	US
Kind code	B2
Filing date	Jan 23, 2007
Priority date	Jan 23, 2007
Publication date	Dec 6, 2016
Grant date	Dec 6, 2016

Abstract

Composite laminates used in structural applications include an interlayer of soft material that provides damping action to reduce noise and vibration. The interlayer may comprise a viscoelastic material which deforms under stress caused by shock, noise or vibration. A reinforcement may be embedded in the viscoelastic material to maintain the mechanical strength and stiffness of the laminate. The reinforcement may include individual or woven fibers or ridged tubes that provide the interlayer with stiffness.

First claim

What is claimed is:

1. A damped composite laminate, comprising:
a first and a second layer comprising a carbon fiber and a resin;
a third layer disposed between the first and second layers, the third layer including damping material comprising a first viscoelastic material having a first glass transition temperature and a reinforcement medium comprising a second viscoelastic material having a second glass transition temperature greater than the first glass transition temperature, the reinforcement medium comprising fiber material, the materials in the third layer different than the resin in the first and second layers; and,
a first barrier layer disposed between and contacting the first layer and the third layer, and a second barrier layer disposed between and contacting the second layer and the third layer, said first and second barrier layers being formed of a fabric of at least 0.0005 inch thick, the first barrier layer and the second barrier layer configured to substantially prevent intermixing of material comprising said first and second layers with material comprising said third layer.

2. The damped composite laminate of claim 1 , wherein all sides of the third layer are surrounded by the first and second layers.

3. The damped composite laminate of claim 1 , wherein the first layer and the second layer are characterized by a plane of orientation, and wherein the reinforcement medium includes fibers embedded in the viscoelastic material, the fibers positioned substantially in the same plane.

4. The damped composite laminate of claim 3 , wherein the fibers are co-cured to the first and second layers.

5. The damped composite laminate of claim 1 , wherein the first layer and the second layer are characterized by a plane of orientation, and wherein the fibers have a length extending a direction generally transverse to the plane of the first and second layers.

6. The damped composite laminate of claim 5 , wherein the fibers are Z-fibers.

7. The damped composite laminate of claim 1 , wherein:
the damping material includes a first viscoelastic material having a first glass transition temperature, and
the reinforcement medium includes fibers impregnated with a second viscoelastic material having a second glass transition temperature greater than the first glass transition temperature.

8. The damped composite laminate of claim 1 , wherein:
the damping material includes a first viscoelastic material having a first glass transition temperature, and
the reinforcement medium includes an open weave of a second viscoelastic material embedded within the first viscoelastic material, the glass transition temperature of the second viscoelastic material being greater than the glass transition temperature of the first viscoelastic material.

9. The damped composite laminate of claim 1 , wherein the reinforcement medium includes inclusions contained within the damping material.

10. The damped composite laminate of claim 9 , wherein the inclusions include one of —
chopped carbon fibers,
fiberous strands,
z-fibers,
a split tape of fiber reinforced resin,
ceramic micro-balloons,
nano-fibers,
nano-tubes.

11. The damped composite laminate of claim 1 , wherein the fiber material of the reinforcement medium includes a net formed of a first viscoelastic material.

12. The damped composite laminate of claim 11 , wherein the damping material is formed of a second viscoelastic, and the net is impregnated with the second viscoelastic material.

13. The damped composite laminate of claim 1 , wherein the reinforcement medium includes rigid connections between the respective barrier layers and third layer.

14. The damped composite laminate of claim 13 , wherein:
the third layer includes perforations, and
the rigid connections include resin disposed within the perforations and extending between the first and second barrier layers.

15. A composite laminate structure, comprising:
at least first and second layers comprising a fiber reinforced with a resin;
a third layer positioned between the first and second layers, the third layer comprising a viscoelastic material having a first glass transition temperature and a fiber reinforcement having a second glass transition temperature greater than the first glass transition temperature, the third layer substantially excluding the resin of the first and second layers; and,
a first barrier layer disposed between and contacting the first layer and the third layer, and a second barrier layer disposed between and contacting the second layer and the third layer, said first and second barrier layers being formed of a thermoplastic fabric preventing intermixing of material comprising said first and second layers with material comprising said third layer.

16. The composite laminate of claim 15 , wherein the viscoelastic material is thermoplastic polyurethane.

17. The composite laminate of claim 15 wherein the fiber reinforcement includes a fiber net extending through the viscoelastic material, generally parallel to the first and second layers.

18. The composite laminate of claim 17 , wherein the fiber net is impregnated with one of a viscoelastic material and an epoxy resin.

19. The composite laminate of claim 15 , wherein the fiber reinforcement includes individual fibers dispersed within the viscoelastic material.

20. The composite laminate of claim 15 , wherein the fiber reinforcement includes a plurality of Z-fibers extending between the first and second barrier layers for reinforcing the viscoelastic material.

21. The composite laminate of claim 15 , wherein the fiber reinforcement is co-cured to the first and second barrier layers.

22. The composite laminate of claim 15 , wherein the third layer is co-cured with the first and second layers.

23. A damped composite laminate, comprising:
a first layer comprising a carbon fiber reinforced with a plastic material;
a second layer comprising a carbon reinforced with the plastic material; and
a third layer disposed between the first and second layers, the third layer including damping material comprising a first viscoelastic material having a first glass transition temperature and a reinforcement medium comprising a second viscoelastic material having a second glass transition temperature greater than the first glass transition temperature, the reinforcement medium comprising fiber material, the third layer substantially excluding the plastic material of the first layer and the second layer.

Assignees

• Montgomery Joshua M
• Liguore Salvatore L
• Cao Tuan Q
• Boeing Co

Inventors

• Montgomery Joshua M
• Liguore Salvatore L
• Cao Tuan Q

Classifications

• B32B5/26

  another layer {next to it} also being fibrous or filamentary {(relative arrangement of fibres or filaments of different layers B32B5/12)} · CPC title

• Y02T50/433

  Cross-Sectional Technologies · mapped topic

• B29C70/44

  using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title

• B32B7/02

  Physical, chemical or physicochemical properties · CPC title

• B29C70/24

  oriented in at least three directions forming a three-dimensional [3D] structure · CPC title